CN114985938B - A method for preparing superhydrophobic surface of aluminum alloy by flat-top laser peening - Google Patents
A method for preparing superhydrophobic surface of aluminum alloy by flat-top laser peening Download PDFInfo
- Publication number
- CN114985938B CN114985938B CN202210641002.3A CN202210641002A CN114985938B CN 114985938 B CN114985938 B CN 114985938B CN 202210641002 A CN202210641002 A CN 202210641002A CN 114985938 B CN114985938 B CN 114985938B
- Authority
- CN
- China
- Prior art keywords
- aluminum alloy
- laser
- carbon powder
- flat
- nano
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 88
- 230000003075 superhydrophobic effect Effects 0.000 title claims abstract description 59
- 241001270131 Agaricus moelleri Species 0.000 title claims abstract description 39
- 238000000034 method Methods 0.000 title claims abstract description 33
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 52
- 239000000463 material Substances 0.000 claims abstract description 25
- 239000000956 alloy Substances 0.000 claims abstract description 17
- 238000010438 heat treatment Methods 0.000 claims abstract description 10
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 8
- 238000010521 absorption reaction Methods 0.000 claims abstract description 7
- 239000011248 coating agent Substances 0.000 claims abstract 2
- 238000000576 coating method Methods 0.000 claims abstract 2
- 239000010410 layer Substances 0.000 claims description 36
- 230000035939 shock Effects 0.000 claims description 6
- 238000005422 blasting Methods 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 5
- 239000003822 epoxy resin Substances 0.000 claims description 4
- 239000003292 glue Substances 0.000 claims description 4
- 229910021392 nanocarbon Inorganic materials 0.000 claims description 4
- 229920000647 polyepoxide Polymers 0.000 claims description 4
- 238000001291 vacuum drying Methods 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 239000008367 deionised water Substances 0.000 claims description 3
- 229910021641 deionized water Inorganic materials 0.000 claims description 3
- 238000001035 drying Methods 0.000 claims description 3
- 238000000227 grinding Methods 0.000 claims description 3
- 238000005498 polishing Methods 0.000 claims description 3
- 238000012545 processing Methods 0.000 claims description 3
- 239000002344 surface layer Substances 0.000 claims description 3
- 230000003746 surface roughness Effects 0.000 claims description 3
- 238000004506 ultrasonic cleaning Methods 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims 1
- 238000005480 shot peening Methods 0.000 abstract description 15
- 230000005661 hydrophobic surface Effects 0.000 abstract description 3
- 238000002360 preparation method Methods 0.000 description 14
- 229910045601 alloy Inorganic materials 0.000 description 7
- 229910001095 light aluminium alloy Inorganic materials 0.000 description 7
- 230000002209 hydrophobic effect Effects 0.000 description 6
- 239000011159 matrix material Substances 0.000 description 6
- 230000008569 process Effects 0.000 description 5
- 238000005096 rolling process Methods 0.000 description 5
- 238000005728 strengthening Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 125000000524 functional group Chemical group 0.000 description 3
- 238000003756 stirring Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000001808 coupling effect Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 239000002086 nanomaterial Substances 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 238000003486 chemical etching Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000002848 electrochemical method Methods 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 229910052731 fluorine Inorganic materials 0.000 description 1
- 239000011737 fluorine Substances 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 238000002309 gasification Methods 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000005416 organic matter Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000003980 solgel method Methods 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/352—Working by laser beam, e.g. welding, cutting or boring for surface treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/14—Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/70—Auxiliary operations or equipment
- B23K26/702—Auxiliary equipment
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/20—Recycling
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Laser Beam Processing (AREA)
Abstract
本发明提供了一种平顶激光喷丸制备铝合金超疏水表面的方法,包括以下步骤:对铝合金表面进行预处理;在预处理后的铝合金表面均匀涂敷纳米级碳粉层;采用方形光斑平顶纳秒脉冲激光,所述碳粉层作为吸收层,对铝合金表面进行无约束层喷丸处理,且光束始终保持与铝合金表面垂直;喷丸后去除残余的碳粉,通过低温热处理降低材料表面能,得到具有微纳多级结构的超疏水铝合金表面。本发明提高了铝合金材料近表层碳元素的含量,可以有效的提高制备疏水表面的硬度及耐磨性。
The invention provides a method for preparing an aluminum alloy superhydrophobic surface by flat-top laser shot peening, comprising the following steps: pretreating the surface of the aluminum alloy; uniformly coating a nano-scale carbon powder layer on the surface of the pretreated aluminum alloy; Square spot flat-top nanosecond pulse laser, the carbon powder layer is used as the absorption layer, and the aluminum alloy surface is subjected to unconstrained layer shot peening, and the beam is always kept perpendicular to the aluminum alloy surface; after the shot peening, the residual carbon powder is removed and passed Low-temperature heat treatment reduces the surface energy of the material, and a superhydrophobic aluminum alloy surface with a micro-nano multilevel structure is obtained. The invention increases the content of carbon element near the surface of the aluminum alloy material, and can effectively improve the hardness and wear resistance of the prepared hydrophobic surface.
Description
技术领域technical field
本发明涉及铝合金超疏水表面制备领域,具体涉及一种平顶激光喷丸制备铝合金超疏水表面的方法。The invention relates to the field of preparation of superhydrophobic surfaces of aluminum alloys, in particular to a method for preparing superhydrophobic surfaces of aluminum alloys by flat-top laser peening.
背景技术Background technique
航空铝合金质量轻、强度高,韧性好,具有优良的力学性能和加工性能,在航空、航天领域应用广泛。航空铝合金表面具有较高的湿润性,使其在低温潮湿的工作环境下产生水滴粘附凝结,材料表面容易发生腐蚀与结冰,对铝合金构件的服役寿命与使用性能产生不利的影响。大量研究表明,在航空铝合金表面构建超疏水结构可以有效的减缓材料表面的腐蚀与结冰,因此,铝合金超疏水表面的制备在航空、航天领域具有重要的意义。Aviation aluminum alloy is light in weight, high in strength, good in toughness, has excellent mechanical properties and processing properties, and is widely used in aviation and aerospace fields. The surface of aviation aluminum alloy has high wettability, which causes water droplets to adhere and condense in a low-temperature and humid working environment. The surface of the material is prone to corrosion and freezing, which will adversely affect the service life and performance of aluminum alloy components. A large number of studies have shown that the construction of superhydrophobic structures on the surface of aerospace aluminum alloys can effectively slow down the corrosion and icing of the material surface. Therefore, the preparation of superhydrophobic surfaces of aluminum alloys is of great significance in the field of aviation and aerospace.
目前,铝合金材料制备超疏水表面的方法多种多样,如电化学法、电花微加工法、化学刻蚀法、电镀法、溶胶-凝胶法等,但这些制备方法存在许多自身缺陷,如工艺复杂、效率低下,其中有些方法需要特殊的设备及严苛的制备环境,使得超疏水表面制备成本高昂,所制备的疏水织构存在强度低,机械稳定性差,制备后基体材料强度降低等问题,这极大地限制了超疏水表面制备工艺在服役环境复杂恶劣的航空铝合金构件上的应用。At present, there are many methods for preparing superhydrophobic surface of aluminum alloy materials, such as electrochemical method, EDM method, chemical etching method, electroplating method, sol-gel method, etc., but these preparation methods have many defects. For example, the process is complex and inefficient, some of which require special equipment and harsh preparation environments, making the preparation of super-hydrophobic surfaces expensive, the prepared hydrophobic texture has low strength, poor mechanical stability, and the strength of the matrix material after preparation. This greatly limits the application of superhydrophobic surface preparation technology on aerospace aluminum alloy components with complex and harsh service environments.
激光喷丸技术作为一种新型的表面改性强化工艺,其利用激光辐照材料表面产生的等离子体冲击波使材料近表层的微观组织发生有益变化,同时在基体内部诱导产生高幅值残余压应力,使材料的力学性能得到有效提高,具有强化效率高,可控性强的优点。利用激光喷丸产生的热力耦合效应可以在航空铝合金表面产生多孔微纳多级结构,降低表面能后赋予铝合金表面超疏水性,是一种重要的超疏水表面制备方式。然而当前激光喷丸制备铝合金超疏水表面的工艺采用的是无吸收层圆形高斯光斑进行喷丸,喷丸时受高斯圆形光斑及搭接率的影响,使制备的超疏水宏观表面具有一定的起伏,液滴的滚动阻力增加,不利于液滴滑移离开材料表面,且在提高制备疏水织构强度方面能力有限。As a new type of surface modification and strengthening process, laser peening technology uses the plasma shock wave generated by laser irradiation on the surface of the material to make beneficial changes in the microstructure of the material near the surface, and at the same time induces high-amplitude residual compressive stress inside the matrix. , so that the mechanical properties of the material are effectively improved, and it has the advantages of high strengthening efficiency and strong controllability. Using the thermal-mechanical coupling effect produced by laser peening can produce porous micro-nano multi-level structure on the surface of aerospace aluminum alloy, and endow the aluminum alloy surface with superhydrophobicity after reducing the surface energy, which is an important superhydrophobic surface preparation method. However, the current process of laser peening to prepare superhydrophobic surface of aluminum alloy adopts circular Gaussian spot without absorbing layer for shot peening, which is affected by Gaussian circular spot and overlap rate during shot peening, so that the prepared superhydrophobic macroscopic surface has With certain undulations, the rolling resistance of the droplets increases, which is not conducive to the sliding of the droplets away from the surface of the material, and has limited ability to improve the strength of the prepared hydrophobic texture.
发明内容Contents of the invention
针对现有技术中存在的不足,本发明提供了一种平顶激光喷丸制备铝合金超疏水表面的方法,在现有激光喷丸制备超疏水表面工艺的基础上,选用方形光斑平顶激光器,以碳粉层作为吸收层进行无约束层喷丸,一方面,激光辐照在碳粉层上增加了对激光能量的吸收率,一部分碳粉吸收激光能量后转化为等离子体,等离子体急剧膨胀产生的冲击波会使受热融化的碳粉与铝合金表面重熔材料进行搅拌调制,提高了铝合金材料近表层碳元素的含量,可以有效的提高制备疏水表面的硬度及耐磨性;另一方面,激光喷丸产生的热力耦合效应使铝合金表面产生具有疏水效果的多孔微纳多级结构的同时使基体材料的微观组织得到有效的强化,力学性能提高。其中方形光斑平顶脉冲激光作为激光冲击的光源,有效改变圆形光斑高斯激光喷丸产生的起伏性形貌,表面平整度提高,可以有效减小液滴的滑动阻力,进一步提高了制备表面的超疏水效果。因此本发明以碳粉层作为吸收层进行无约束层方形光斑平顶脉冲激光喷丸,在铝合金材料基体上高效完成超疏水表面制备的同时实现了基体材料的强化,超疏水效果及表面强度也得到有效提高,超疏水表面机械耐磨性增强。Aiming at the deficiencies in the prior art, the present invention provides a method for preparing a superhydrophobic surface of an aluminum alloy by flat-top laser peening. On the basis of the existing technology for preparing a superhydrophobic surface by laser peening, a flat-top laser with a square spot is selected. , the carbon powder layer is used as the absorbing layer for unconstrained layer shot peening. On the one hand, the laser irradiation increases the absorption rate of laser energy on the carbon powder layer, and a part of the carbon powder absorbs the laser energy and converts into plasma, and the plasma rapidly The shock wave generated by the expansion will stir and modulate the heated and melted carbon powder and the remelted material on the surface of the aluminum alloy, increasing the content of carbon elements near the surface of the aluminum alloy material, which can effectively improve the hardness and wear resistance of the prepared hydrophobic surface; another On the one hand, the thermal-mechanical coupling effect produced by laser peening produces a porous micro-nano multi-level structure with a hydrophobic effect on the surface of the aluminum alloy, and at the same time effectively strengthens the microstructure of the matrix material and improves the mechanical properties. Among them, the square spot flat-top pulse laser is used as the light source of laser shock, which can effectively change the undulating shape of the circular spot Gaussian laser peening, improve the surface flatness, effectively reduce the sliding resistance of the droplet, and further improve the prepared surface. superhydrophobic effect. Therefore, the present invention uses the carbon powder layer as the absorbing layer to perform unconstrained layer square spot flat-top pulse laser peening, and efficiently completes the preparation of the super-hydrophobic surface on the aluminum alloy substrate while realizing the strengthening of the substrate material, super-hydrophobic effect and surface strength. It is also effectively improved, and the mechanical wear resistance of the superhydrophobic surface is enhanced.
本发明是通过以下技术手段实现上述技术目的的。The present invention achieves the above-mentioned technical purpose through the following technical means.
一种平顶激光喷丸制备铝合金超疏水表面的方法,包括以下步骤:A method for preparing an aluminum alloy superhydrophobic surface by flat-top laser peening, comprising the following steps:
对铝合金表面进行预处理;Pretreatment of aluminum alloy surface;
在预处理后的铝合金表面均匀涂敷纳米级碳粉层;Evenly coat the nano-scale carbon powder layer on the surface of the pretreated aluminum alloy;
采用方形光斑平顶纳秒脉冲激光,所述碳粉层作为吸收层,对铝合金表面进行无约束层喷丸处理,且光束始终保持与铝合金表面垂直;Using a square spot flat-top nanosecond pulse laser, the carbon powder layer is used as an absorbing layer, and the surface of the aluminum alloy is subjected to unconstrained layer shot peening, and the beam is always kept perpendicular to the surface of the aluminum alloy;
喷丸后去除残余的碳粉,通过低温热处理降低材料表面能,得到具有微纳多级结构的超疏水铝合金表面。After shot peening, the residual carbon powder is removed, and the surface energy of the material is reduced by low-temperature heat treatment to obtain a superhydrophobic aluminum alloy surface with a micro-nano multi-level structure.
进一步,所述预处理包括:对铝合金表面进行逐级打磨抛光,使表面粗糙度值≤50μm,采用去离子水对处理后表面进行超声清洗并烘干。Further, the pretreatment includes: grinding and polishing the surface of the aluminum alloy step by step to make the surface roughness ≤ 50 μm, ultrasonically cleaning and drying the treated surface with deionized water.
进一步,所述纳米级碳粉层为纳米碳粉与环氧树脂胶的混合物,所述纳米碳粉的直径范围为50nm~300nm,所述纳米级碳粉层厚度为100μm~500μm。Further, the nanoscale carbon powder layer is a mixture of nanoscale carbon powder and epoxy resin glue, the diameter of the nanoscale carbon powder ranges from 50 nm to 300 nm, and the thickness of the nanoscale carbon powder layer is 100 μm to 500 μm.
进一步,所述方形光斑平顶纳秒脉冲激光由圆形平顶纳秒脉冲激光通过光束整形器得到。Further, the flat-top nanosecond pulsed laser with a square spot is obtained by passing a circular flat-top nanosecond pulsed laser through a beam shaper.
进一步,产生方形光斑平顶纳秒脉冲激光的激光器为Nd:YAG固体激光器,激光器加工参数为:波长1064nm,激光能量1J~15J,重复频率1Hz~5Hz,脉冲宽度10ns~20ns,方形光斑边长尺寸≤5mm。Further, the laser that produces flat-top nanosecond pulse laser with square spot is Nd:YAG solid-state laser, and the laser processing parameters are: wavelength 1064nm, laser energy 1J~15J, repetition frequency 1Hz~5Hz, pulse width 10ns~20ns, square spot side length Size≤5mm.
进一步,所述低温热处理降低材料表面能的方法为:将喷丸处理后的铝合金材料置于80℃~150℃的真空干燥箱中进行处理,处理时间为1h~10h。Further, the method for lowering the surface energy of the material by the low-temperature heat treatment is as follows: placing the aluminum alloy material after the shot blasting treatment in a vacuum drying oven at 80° C. to 150° C. for 1 h to 10 h.
本发明的有益效果在于:The beneficial effects of the present invention are:
1.本发明所述的平顶激光喷丸制备铝合金超疏水表面的方法,选用方形光斑平顶脉冲激光,相对于传统的圆形光斑高斯脉冲激光在喷丸过程中,应力波以纵向传播的平面压缩波为主,表面横向波所占能量比重较低,基于这种特征,方形平顶光斑激光喷丸的各邻近喷丸点所诱导的残余应力场之间不会产生复杂的干涉作用,喷丸先后顺序导致的应力应变场不均匀性将被大大削弱,避免了圆形光斑高斯脉冲激光喷丸时产生的应力空洞现象,喷丸处理后宏观表面形貌较平坦,有利于提高制备表面的疏水效果,且基体材料残余压应力场分布更加均匀,材料的服役寿命得到延长。1. The method for preparing the superhydrophobic surface of aluminum alloy by flat-top laser shot peening of the present invention selects square spot flat-top pulse laser for use. Compared with the traditional circular spot Gaussian pulse laser in the shot peening process, the stress wave propagates in the longitudinal direction Based on this feature, the residual stress field induced by each adjacent shot peening point of the square flat-top spot laser peening will not produce complex interference. , the inhomogeneity of the stress-strain field caused by the sequence of shot peening will be greatly weakened, avoiding the stress cavity phenomenon caused by circular spot Gaussian pulse laser peening, and the macroscopic surface morphology after shot peening is relatively flat, which is conducive to improving the preparation The hydrophobic effect of the surface, and the distribution of the residual compressive stress field of the matrix material is more uniform, and the service life of the material is prolonged.
2.本发明所述的平顶激光喷丸制备铝合金超疏水表面的方法,使用碳粉层充当激光喷丸时的吸收层,当高功率密度的强脉冲激光辐照在铝合金板料表面时,碳粉吸收部分能量致使迅速电离气化,继续吸收激光能量生成高压冲击波使融化的碳粉与铝合金表层重熔材料发生搅拌调制,铝合金近表层的碳含量上升,有效提高了疏水微纳织构的硬度,使得制备的超疏水表面具有较好的耐磨性;同时,在激光喷丸力效应的作用下,金属材料表层形成了较高的位错密度,晶粒也得到了有效细化,织构表面的摩擦磨损性能和机械稳定性提高。2. The method for preparing the superhydrophobic surface of aluminum alloy by flat-top laser peening according to the present invention uses a carbon powder layer as the absorbing layer during laser peening, when the intense pulsed laser radiation with high power density is irradiated on the surface of the aluminum alloy sheet At this time, the carbon powder absorbs part of the energy to cause rapid ionization and gasification, and continues to absorb laser energy to generate high-voltage shock waves to stir and modulate the melted carbon powder and the remelted material on the surface of the aluminum alloy. The carbon content near the surface of the aluminum alloy increases, effectively improving the hydrophobic micro The hardness of the nanotexture makes the prepared superhydrophobic surface have better wear resistance; at the same time, under the effect of laser peening force, the surface layer of the metal material forms a higher dislocation density, and the grains are also effectively The refined, textured surface has improved friction and wear properties and mechanical stability.
3.本发明所述的平顶激光喷丸制备铝合金超疏水表面的方法,利用低温热处理工艺降低具有微纳多级结构表面的表面能,清洁无污染。低温热处理使试样表面与空气中的氧气发生较充分的作用,对微纳多级结构表面的成分进行调控,显著提高铝合金表面对空气中有机物的吸附能力,结合激光喷丸过程中在微纳多级织构中引入的大量碳元素,材料表面非极性官能团大量增加,表面能得到有效降低,实现了无氟铝合金超疏水表面的制备。3. The method for preparing an aluminum alloy superhydrophobic surface by flat-top laser peening according to the present invention uses a low-temperature heat treatment process to reduce the surface energy of a surface with a micro-nano multi-level structure, which is clean and pollution-free. The low-temperature heat treatment makes the surface of the sample fully interact with the oxygen in the air, regulates the composition of the surface of the micro-nano multi-level structure, and significantly improves the adsorption capacity of the aluminum alloy surface to the organic matter in the air. The introduction of a large amount of carbon elements in the nanoscale texture increases the non-polar functional groups on the surface of the material, effectively reduces the surface energy, and realizes the preparation of the superhydrophobic surface of the fluorine-free aluminum alloy.
4.本发明所述的平顶激光喷丸制备铝合金超疏水表面的方法,具有操作简便,成本低廉等优点,易于实现大规模工业化生产,显著提高了超疏水表面微纳多级织构的耐磨性与机械稳定性,铝合金基体材料强度也得到一定提高,更好的适用于航天航空领域复杂严苛的环境,具有较为广泛的工业应用前景。4. The method for preparing the superhydrophobic surface of aluminum alloy by flat-top laser peening according to the present invention has the advantages of simple and convenient operation, low cost, etc., is easy to realize large-scale industrial production, and significantly improves the micro-nano multi-level texture of the superhydrophobic surface. Wear resistance and mechanical stability, and the strength of the aluminum alloy matrix material have also been improved to a certain extent, which is better suitable for the complex and harsh environment in the aerospace field, and has a wide range of industrial application prospects.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,下面描述中的附图是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,显而易见地还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. For some embodiments, it is obvious to those skilled in the art that other drawings can be obtained based on these drawings without any creative effort.
图1为本发明所述的平顶激光喷丸制备铝合金超疏水表面的方法原理图。Fig. 1 is a schematic diagram of the method for preparing an aluminum alloy superhydrophobic surface by flat-top laser peening according to the present invention.
图2为本发明实施例一制备的超疏水表面形貌实际效果图。Fig. 2 is an actual effect diagram of the superhydrophobic surface morphology prepared in Example 1 of the present invention.
图3为本发明各实施例制备的超疏水表面液滴接触角对比图。Fig. 3 is a comparison diagram of contact angles of droplets on superhydrophobic surfaces prepared in various embodiments of the present invention.
图4为本发明各实施例制备的超疏水表面显微硬度对比图。Fig. 4 is a comparison chart of microhardness of superhydrophobic surfaces prepared in various embodiments of the present invention.
图5为本发明实施例三制备的超疏水表面经过不同时长超声振动处理液滴接触角变化曲线图。Fig. 5 is a graph showing the variation of droplet contact angles of the superhydrophobic surface prepared in Example 3 of the present invention after ultrasonic vibration treatment for different durations.
具体实施方式detailed description
下面结合附图以及具体实施例对本发明作进一步的说明,但本发明的保护范围并不限于此。The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments, but the protection scope of the present invention is not limited thereto.
下面详细描述本发明的实施例,所述实施例的示例在附图中示出,其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention.
在本发明的描述中,需要理解的是,术语“中心”、“纵向”、“横向”、“长度”、“宽度”、“厚度”、“上”、“下”、“轴向”、“径向”、“竖直”、“水平”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。此外,术语“第一”、“第二”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括一个或者更多个该特征。在本发明的描述中,“多个”的含义是两个或两个以上,除非另有明确具体的限定。In describing the present invention, it is to be understood that the terms "central", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "axial", The orientation or positional relationship indicated by "radial", "vertical", "horizontal", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description , rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and thus should not be construed as limiting the invention. In addition, the terms "first" and "second" are used for descriptive purposes only, and cannot be interpreted as indicating or implying relative importance or implicitly specifying the quantity of indicated technical features. Thus, a feature defined as "first" and "second" may explicitly or implicitly include one or more of these features. In the description of the present invention, "plurality" means two or more, unless otherwise specifically defined.
在本发明中,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”、“固定”等术语应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明中的具体含义。In the present invention, unless otherwise clearly specified and limited, terms such as "installation", "connection", "connection" and "fixation" should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection , or integrally connected; it may be mechanically connected or electrically connected; it may be directly connected or indirectly connected through an intermediary, and it may be the internal communication of two components. Those of ordinary skill in the art can understand the specific meanings of the above terms in the present invention according to specific situations.
如图1所示,本发明所述的平顶激光喷丸制备铝合金超疏水表面的方法,包括如下步骤:As shown in Figure 1, the method for preparing an aluminum alloy superhydrophobic surface by flat-top laser peening of the present invention comprises the following steps:
对铝合金表面进行逐级打磨抛光,使表面粗糙度值≤50μm,并采用去离子水对处理后表面进行超声清洗并烘干;The surface of the aluminum alloy is polished and polished step by step to make the surface roughness ≤ 50 μm, and the treated surface is ultrasonically cleaned and dried with deionized water;
将直径范围为50nm~300nm的纳米碳粉与环氧树脂胶混合涂敷在铝合金板材表面,在铝合金表面形成厚度为100μm~500μm的纳米级碳粉层;Mix and coat nano-carbon powder with a diameter ranging from 50nm to 300nm and epoxy resin glue on the surface of the aluminum alloy plate to form a nano-scale carbon powder layer with a thickness of 100 μm to 500 μm on the surface of the aluminum alloy;
采用方形光斑平顶纳秒脉冲激光器,选用合理的参数及路径以所述碳粉层充当激光喷丸时的吸收层,对铝合金试样表面进行无约束层喷丸处理,且光束始终保持与板材表面垂直;Using a square spot flat-top nanosecond pulse laser, selecting reasonable parameters and paths, using the carbon powder layer as the absorbing layer during laser peening, performing unconstrained layer shot peening on the surface of the aluminum alloy sample, and the beam is always kept in line with The surface of the plate is vertical;
喷丸结束后使用超声清洗去除铝合金表面的残余碳粉,随后将喷丸处理后的板材置于恒温80℃~150℃的真空干燥箱中进行低温处理,时间为1h~10h,以降低材料的表面能,完成具有微纳多级结构的超疏水铝合金表面的制备。After the shot peening, use ultrasonic cleaning to remove the residual carbon powder on the surface of the aluminum alloy, and then place the shot peened plate in a vacuum drying oven with a constant temperature of 80°C to 150°C for low temperature treatment for 1h to 10h to reduce the material Surface energy, complete the preparation of superhydrophobic aluminum alloy surface with micro-nano multi-level structure.
本发明所述的平顶激光喷丸制备铝合金超疏水表面的方法,通过光束整形器将圆形光斑平顶纳秒脉冲激光转变为方形光斑平顶纳秒脉冲激光,以纳米级碳粉层为吸收层,在铝合金表面进行无约束层激光喷丸,结合低温热处理工艺降低材料表面能,赋予铝合金表面超疏水性。运用方形光斑平顶脉冲激光进行喷丸,有利于对激光喷丸产生的残余压应力进行调控,使应力分布更加均匀,可以有效提高材料的服役寿命;以纳米级碳粉作为激光喷丸时的吸收层,激光能量的吸收率增加,产生高强度的等离子冲击波,对材料起到冲击强化的同时将融化的碳粉与铝合金表面重熔物质进行搅拌,大幅提高铝合金表层碳元素的含量,进而提高了制备多级微纳结构的强度和硬度,使得制备的超疏水表面具有较高的基体耐磨性与机械稳定性;通过对激光光斑尺寸形状、激光能量、搭接率及喷丸路径等参数的优化设置可以实现对激光喷丸制备的超疏水表面宏观形貌进行调控,使得制备表面较平坦,可以有效的减小液滴滑动的阻力,滚动角减小;本发明中采用低温热处理处理的方式在铝合金材料表面引入大量的非极性官能团,实现了对制备的微纳多级结构表面能的降低,采用无氟添加的方式实现了铝合金超疏水表面的制备。The method for preparing the superhydrophobic surface of aluminum alloy by flat-top laser peening described in the present invention converts the circular spot flat-top nanosecond pulse laser into a square spot flat-top nanosecond pulse laser through a beam shaper, and uses nano-scale carbon powder layer For the absorbing layer, unconstrained layer laser peening is performed on the surface of the aluminum alloy, combined with a low-temperature heat treatment process to reduce the surface energy of the material, and endow the aluminum alloy surface with superhydrophobicity. The use of square-spot flat-top pulsed laser for peening is beneficial to control the residual compressive stress generated by laser peening, making the stress distribution more uniform and effectively improving the service life of materials; when using nano-scale carbon powder as the Absorbing layer, the absorption rate of laser energy is increased to generate high-intensity plasma shock waves, which can impact the material while stirring the melted carbon powder and the remelted material on the surface of the aluminum alloy, greatly increasing the content of carbon elements on the surface of the aluminum alloy. In turn, the strength and hardness of the prepared multi-level micro-nano structure are improved, so that the prepared superhydrophobic surface has high matrix wear resistance and mechanical stability; The optimal setting of parameters such as laser peening can realize the regulation and control of the macroscopic morphology of the superhydrophobic surface prepared by laser peening, so that the prepared surface is relatively flat, which can effectively reduce the resistance of the droplet sliding, and the rolling angle is reduced; in the present invention, low temperature heat treatment is used The treatment method introduces a large number of non-polar functional groups on the surface of the aluminum alloy material, which reduces the surface energy of the prepared micro-nano multi-level structure, and realizes the preparation of the superhydrophobic surface of the aluminum alloy by adopting a method without fluorine addition.
为使本发明的目的、技术方案和优点更加清楚,下面选取2024-T351航空铝合金作为研究对象,结合具体实施例对本发明进行详细的描述。In order to make the purpose, technical solution and advantages of the present invention clearer, 2024-T351 aviation aluminum alloy is selected as the research object below, and the present invention will be described in detail in conjunction with specific examples.
实施例一:Embodiment one:
实施例一所述的平顶激光喷丸制备铝合金超疏水表面的方法,包括如下步骤:The method for preparing the superhydrophobic surface of aluminum alloy by flat-top laser peening described in embodiment one may further comprise the steps:
(1)将2024-T351航空铝合金表面使用400#、800#、1000#、1500#、2000#粒径的砂纸进行打磨,并在磨抛机上进行抛光,使铝合金材料表面达到镜面(Ra≤50μm),然后在无水乙醇溶液中对试样表面进行超声清洗5min,在真空干燥箱中烘干备用;(1) Grind the surface of 2024-T351 aviation aluminum alloy with 400#, 800#, 1000#, 1500#, 2000# grain size sandpaper, and polish it on a grinding and polishing machine, so that the surface of the aluminum alloy material reaches a mirror surface (Ra ≤50μm), then ultrasonically clean the surface of the sample in absolute ethanol solution for 5 minutes, and dry it in a vacuum drying oven for later use;
(2)将直径为50nm的碳粉与环氧树脂胶混合涂敷在铝合金板材表面,在铝合金表面形成厚度为100μm的纳米碳粉层;(2) Mix carbon powder with a diameter of 50 nm and epoxy resin glue on the surface of the aluminum alloy plate, and form a nano carbon powder layer with a thickness of 100 μm on the surface of the aluminum alloy;
(3)选用Nd:YAG高重频大能量纳秒脉冲激光器,调整光束整形器,使圆形光斑平顶脉冲纳秒激光转变为方形光斑平顶脉冲纳秒激光,激光喷丸具体参数为:波长1064nm,激光频率1Hz,脉冲宽度20ns,光斑搭接率0%,光斑直径3mm,激光能量5J;(3) Select Nd:YAG high-repetition frequency and high-energy nanosecond pulse laser, adjust the beam shaper, so that the circular spot flat-top pulse nanosecond laser is transformed into a square spot flat-top pulse nanosecond laser. The specific parameters of laser peening are: Wavelength 1064nm, laser frequency 1Hz, pulse width 20ns,
(4)激光喷丸结束后使用超声清洗去除铝合金表面的残余碳粉,将航空铝合金试样放置在温度为100℃的烘干箱中进行低温热处理5h,在铝合金材料表面引入大量的非极性官能团,降低铝合金材料的表面能,完成铝合金超疏水表面的制备。(4) After laser peening, use ultrasonic cleaning to remove residual carbon powder on the surface of the aluminum alloy, place the aviation aluminum alloy sample in a drying oven at a temperature of 100°C for 5 hours of low-temperature heat treatment, and introduce a large amount of carbon powder on the surface of the aluminum alloy material The non-polar functional group reduces the surface energy of the aluminum alloy material and completes the preparation of the superhydrophobic surface of the aluminum alloy.
实施例一制备的航空铝合金超疏水表面的形貌如图2所示,相对于圆形光斑高斯脉冲纳秒激光制备的铝合金超疏水表面,试样宏观表面较平坦,同时具有优异的微纳多级结构形貌,提高了制备表面的疏水效果;如图3所示,实施例一制备的试样表面具有优异的超疏水性,液滴滑动阻力较小,液滴接触角为162°,滚动角为4°;如图4所示,在激光喷丸产生的热力作用下,航空铝合金表层的碳元素大量增加,极大地提升了制备的航空铝合金超疏水表面的显微硬度,达到了191HV,相较于未处理试样表面的平均硬度值130HV提升了46.9%,这对提高制备超疏水表面的耐磨损性具有重要的意义。The morphology of the superhydrophobic surface of the aerospace aluminum alloy prepared in Example 1 is shown in Figure 2. Compared with the superhydrophobic surface of the aluminum alloy prepared by the circular spot Gaussian pulse nanosecond laser, the macroscopic surface of the sample is relatively flat and has excellent microscopic properties. The nanoscale structure morphology improves the hydrophobic effect of the prepared surface; as shown in Figure 3, the surface of the sample prepared in Example 1 has excellent superhydrophobicity, the droplet sliding resistance is small, and the droplet contact angle is 162° , the rolling angle is 4°; as shown in Figure 4, under the heat generated by laser peening, the carbon element in the surface layer of aviation aluminum alloy increases greatly, which greatly improves the microhardness of the superhydrophobic surface of the prepared aviation aluminum alloy. It has reached 191HV, which is 46.9% higher than the average hardness value of 130HV on the surface of the untreated sample, which is of great significance for improving the wear resistance of the prepared superhydrophobic surface.
实施例二Embodiment two
在实施例一的基础上,实施例二中的碳粉直径达到300nm,碳粉吸收层厚度为500μm,激光喷丸能量设置为13J。On the basis of Example 1, the diameter of the carbon powder in Example 2
如图3所示,实施例二得到的超疏水表面的液滴接触角为159°,滚动角为5°,同样实现了航空铝合金表面的优异超疏水性。实施例二采用了更大的碳粉颗粒与更厚的碳粉吸收层,激光喷丸能量也提高了,在航空铝合金表面产生的更深的影响层,强化效果也得到了有效提高,如图4所示,本实施例制备的航空铝合金超疏水表面显微硬度值为211HV,相较于未处理试样基体材料表面的平均硬度130HV提升了62.3%,相较于实施例一处理后试样表面的平均硬度HV191提升了10.5%,更多的碳粉、更大的激光能量使得碳元素与铝合金表面的重熔物质搅拌更充分,超疏水表面的硬度和机械稳定性进一步提高。As shown in Figure 3, the droplet contact angle of the superhydrophobic surface obtained in Example 2 is 159°, and the rolling angle is 5°, which also realizes the excellent superhydrophobicity of the aerospace aluminum alloy surface. Embodiment 2 uses larger carbon powder particles and thicker carbon powder absorption layer, and the energy of laser peening is also increased. The deeper impact layer produced on the surface of aviation aluminum alloy, the strengthening effect is also effectively improved, as shown in the figure As shown in 4, the microhardness value of the superhydrophobic surface of the aerospace aluminum alloy prepared in this embodiment is 211HV, which is 62.3% higher than the average hardness of 130HV on the surface of the untreated sample base material. The average hardness HV191 of the sample surface increased by 10.5%. More carbon powder and greater laser energy made the carbon element and the remelted material on the aluminum alloy surface more fully stirred, and the hardness and mechanical stability of the superhydrophobic surface were further improved.
实施例三Embodiment three
在实施例一的基础上,实施例三中的碳粉直径150nm,碳粉吸收层厚度300μm,激光喷丸能量设置为8J。On the basis of Example 1, the diameter of the carbon powder in Example 3 is 150 nm, the thickness of the carbon powder absorption layer is 300 μm, and the laser peening energy is set to 8J.
实施例三处理的试样表面液滴接触角为164°,滚动角为4°,所制备的航空铝合金试样表面同样具有优异的超疏水性能,本实施例制备的航空铝合金超疏水表面显微硬度值为201HV,相较于未处理试样基体材料表面的平均硬度130HV提升了54.6%。将实施例三制备的试样置于超声振动台上进行疏水表面稳定性表征实验,如图5所示,随着振动时间的增加,制备的超疏水表面液滴接触角有所下降,但5个小时后依然保持在155°以上,可以看出所制备的航空铝合金超疏水表面具有较高的机械稳定性。The droplet contact angle of the sample surface treated in Example 3 is 164°, and the rolling angle is 4°. The surface of the prepared aviation aluminum alloy sample also has excellent superhydrophobic properties. The aviation aluminum alloy superhydrophobic surface prepared in this example The microhardness value is 201HV, which is 54.6% higher than the average hardness of 130HV on the surface of the untreated sample base material. The sample prepared in Example 3 was placed on an ultrasonic vibration table to carry out a hydrophobic surface stability characterization experiment. As shown in Figure 5, as the vibration time increased, the droplet contact angle of the prepared superhydrophobic surface decreased, but 5 Hours later, it still remains above 155°, which shows that the prepared aerospace aluminum alloy superhydrophobic surface has high mechanical stability.
应当理解,虽然本说明书是按照各个实施例描述的,但并非每个实施例仅包含一个独立的技术方案,说明书的这种叙述方式仅仅是为清楚起见,本领域技术人员应当将说明书作为一个整体,各实施例中的技术方案也可以经适当组合,形成本领域技术人员可以理解的其他实施方式。It should be understood that although this description is described according to various embodiments, not each embodiment only includes an independent technical solution, and this description of the description is only for clarity, and those skilled in the art should take the description as a whole , the technical solutions in the various embodiments can also be properly combined to form other implementations that can be understood by those skilled in the art.
上文所列出的一系列的详细说明仅仅是针对本发明的可行性实施例的具体说明,它们并非用以限制本发明的保护范围,凡未脱离本发明技艺精神所作的等效实施例或变更均应包含在本发明的保护范围之内。The series of detailed descriptions listed above are only specific descriptions for feasible embodiments of the present invention, and they are not intended to limit the protection scope of the present invention. Any equivalent embodiment or All changes should be included within the protection scope of the present invention.
Claims (6)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210641002.3A CN114985938B (en) | 2022-06-08 | 2022-06-08 | A method for preparing superhydrophobic surface of aluminum alloy by flat-top laser peening |
GB2313401.8A GB2623639A (en) | 2022-06-08 | 2022-07-18 | Method for preparing aluminum alloy super-hydrophobic surface by flat-top laser peening |
US18/010,839 US11839934B1 (en) | 2022-06-08 | 2022-07-18 | Method for preparing super-hydrophobic aluminum alloy surface through flat-topped laser peening |
PCT/CN2022/106171 WO2023236314A1 (en) | 2022-06-08 | 2022-07-18 | Method for preparing aluminum alloy super-hydrophobic surface by flat-top laser peening |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210641002.3A CN114985938B (en) | 2022-06-08 | 2022-06-08 | A method for preparing superhydrophobic surface of aluminum alloy by flat-top laser peening |
Publications (2)
Publication Number | Publication Date |
---|---|
CN114985938A CN114985938A (en) | 2022-09-02 |
CN114985938B true CN114985938B (en) | 2023-01-17 |
Family
ID=83033004
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210641002.3A Active CN114985938B (en) | 2022-06-08 | 2022-06-08 | A method for preparing superhydrophobic surface of aluminum alloy by flat-top laser peening |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN114985938B (en) |
WO (1) | WO2023236314A1 (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006320907A (en) * | 2005-05-17 | 2006-11-30 | Muneharu Kutsuna | Micro laser peening treatment and parts using micro laser peening treatment using powder and coating |
CN104947116A (en) * | 2015-05-28 | 2015-09-30 | 湖北工业大学 | Method for preparing aluminum alloy superhydrophobic self-cleaning surface by using ultrashort pulse laser |
CN106112268A (en) * | 2016-07-22 | 2016-11-16 | 广东工业大学 | A kind of band muscle wallboard laser shot forming system and method |
CN106191384A (en) * | 2016-07-13 | 2016-12-07 | 广东工业大学 | Metal blank laser shot forming dynamic self-adapting equipment based on guide rail motion and method |
EP3147048A1 (en) * | 2015-09-28 | 2017-03-29 | Ecole Polytechnique Federale De Lausanne (Epfl) | Method and device for implementing laser shock peening (lsp) or warm laser shock peening (wlsp) during selective laser melting (slm) |
CN107099656A (en) * | 2017-06-29 | 2017-08-29 | 西北有色金属研究院 | A preparation method of laser shock absorbing layer for titanium alloy |
CN112375899A (en) * | 2020-10-29 | 2021-02-19 | 上海交通大学 | Rectangular uniform laser pulse shock strengthening and forming system and application method thereof |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4058448B2 (en) * | 2005-12-26 | 2008-03-12 | 宗春 沓名 | Laser peening treatment method and laser absorbing powder layer sheet |
CN104164538B (en) * | 2014-07-16 | 2017-02-22 | 江苏大学 | Laser shock reinforcing method for obtaining large area uniform surface morphology |
CN105039652B (en) * | 2015-04-29 | 2017-09-05 | 江苏大学 | A Square Spot Laser Shock Uniform Strengthening Method for Curved Surfaces |
CN106119467B (en) * | 2016-07-26 | 2018-06-12 | 广东工业大学 | A kind of method and apparatus for controlling laser peening parameter monitoring blade surface roughness |
CN111468831A (en) * | 2019-01-23 | 2020-07-31 | 中国科学院长春光学精密机械与物理研究所 | Self-cleaning metal surface, its preparation method and processing device |
CN109880998B (en) * | 2019-03-01 | 2020-11-13 | 广东工业大学 | Method and device for monitoring surface profile of blade |
CN113967796B (en) * | 2021-10-26 | 2023-09-22 | 江苏大学 | A method for preparing superhydrophobic surface by laser shock imprinting micro-nano particles on aluminum alloy surface |
CN114406475B (en) * | 2021-12-01 | 2023-09-22 | 江苏大学 | A method for preparing aluminum alloy superhydrophobic surface by laser shot peening |
-
2022
- 2022-06-08 CN CN202210641002.3A patent/CN114985938B/en active Active
- 2022-07-18 WO PCT/CN2022/106171 patent/WO2023236314A1/en active Application Filing
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006320907A (en) * | 2005-05-17 | 2006-11-30 | Muneharu Kutsuna | Micro laser peening treatment and parts using micro laser peening treatment using powder and coating |
CN104947116A (en) * | 2015-05-28 | 2015-09-30 | 湖北工业大学 | Method for preparing aluminum alloy superhydrophobic self-cleaning surface by using ultrashort pulse laser |
EP3147048A1 (en) * | 2015-09-28 | 2017-03-29 | Ecole Polytechnique Federale De Lausanne (Epfl) | Method and device for implementing laser shock peening (lsp) or warm laser shock peening (wlsp) during selective laser melting (slm) |
CN106191384A (en) * | 2016-07-13 | 2016-12-07 | 广东工业大学 | Metal blank laser shot forming dynamic self-adapting equipment based on guide rail motion and method |
CN106112268A (en) * | 2016-07-22 | 2016-11-16 | 广东工业大学 | A kind of band muscle wallboard laser shot forming system and method |
CN107099656A (en) * | 2017-06-29 | 2017-08-29 | 西北有色金属研究院 | A preparation method of laser shock absorbing layer for titanium alloy |
CN112375899A (en) * | 2020-10-29 | 2021-02-19 | 上海交通大学 | Rectangular uniform laser pulse shock strengthening and forming system and application method thereof |
Also Published As
Publication number | Publication date |
---|---|
WO2023236314A1 (en) | 2023-12-14 |
CN114985938A (en) | 2022-09-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN114406475B (en) | A method for preparing aluminum alloy superhydrophobic surface by laser shot peening | |
CN108515269B (en) | A method for direct preparation of stainless steel superhydrophobic self-cleaning surface by picosecond laser | |
US11839934B1 (en) | Method for preparing super-hydrophobic aluminum alloy surface through flat-topped laser peening | |
CN114507468B (en) | Photothermal self-healing coating on magnesium alloy surface and preparation method thereof | |
CN114682922B (en) | A method for controlling the stress and texture morphology of superhydrophobic surface of aluminum alloy prepared by laser etching | |
CN109107226A (en) | A kind of metal mesh for oil-water separation preparation method that wetability is controllable | |
CN104907697B (en) | A method for preparing titanium alloy superhydrophobic frost-resistant surface by ultrafast laser | |
CN103849757A (en) | Laser induction cavitation-based metal surface strengthening device and method | |
CN113967796B (en) | A method for preparing superhydrophobic surface by laser shock imprinting micro-nano particles on aluminum alloy surface | |
CN104947035A (en) | Method for enabling metal surface to penetrate nano powder by laser-induced impact | |
CN114985938B (en) | A method for preparing superhydrophobic surface of aluminum alloy by flat-top laser peening | |
CN113308600B (en) | Hydrophobic coating based laser shock method | |
CN111518474A (en) | Photo-thermal deicing surface coating and preparation method thereof | |
CN114799532B (en) | Laser irradiation combined with wax seal polishing method to prepare high-quality amorphous alloy micro-pits | |
CN111525086A (en) | Preparation method of lithium battery electrode based on laser shock technology | |
CN210974824U (en) | Material strengthening device for underwater particle-cavitation coupling | |
CN114952010B (en) | Pulse current assisted aluminum alloy laser shot-peening forming and hydrophobic surface preparation method | |
CN112708915B (en) | Micro-arc aluminum oxide alloy material | |
CN115074721A (en) | Preparation process of high-flux tube porous coating | |
CN115433988A (en) | Method for improving corrosion resistance of magnesium alloy by synchronous laser-micro arc oxidation compounding | |
CN102912309A (en) | Method for improving cavitation erosion resistance of TC4 titanium alloy based on ion implantation surface modification | |
CN108559992A (en) | Preparation method of multi-scale metal ceramic solar selective absorption coating | |
CN119662056B (en) | Preparation method and application of alumina-doped high-temperature radar absorbing coating | |
CN112725860B (en) | Simple micro-arc oxidation aluminum material treatment method | |
CN117431495B (en) | Super-hydrophobic anti-corrosion double-layer structure of metal surface and preparation method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |